BE685664A - - Google Patents

Info

Publication number
BE685664A
BE685664A BE685664DA BE685664A BE 685664 A BE685664 A BE 685664A BE 685664D A BE685664D A BE 685664DA BE 685664 A BE685664 A BE 685664A
Authority
BE
Belgium
Application number
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Publication of BE685664A publication Critical patent/BE685664A/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BE685664D 1965-12-06 1966-08-18 BE685664A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US511865A US3302926A (en) 1965-12-06 1965-12-06 Segmented nozzle diaphragm for high temperature turbine

Publications (1)

Publication Number Publication Date
BE685664A true BE685664A (en) 1967-02-01

Family

ID=24036770

Family Applications (1)

Application Number Title Priority Date Filing Date
BE685664D BE685664A (en) 1965-12-06 1966-08-18

Country Status (4)

Country Link
US (1) US3302926A (en)
BE (1) BE685664A (en)
DE (1) DE1476795B2 (en)
GB (1) GB1129410A (en)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2121707C3 (en) * 1971-05-03 1974-06-20 Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen Guide vane ring
US3898883A (en) * 1972-01-17 1975-08-12 Kozak Zdenek Stator assembly for flowmeters and the like
GB1385666A (en) * 1973-07-06 1975-02-26 Rolls Royce Sealing of vaned assemblies of gas turbine engines
US3918832A (en) * 1974-07-29 1975-11-11 United Technologies Corp Stator construction for an axial flow compressor
US4015910A (en) * 1976-03-09 1977-04-05 The United States Of America As Represented By The Secretary Of The Air Force Bolted paired vanes for turbine
GB1605297A (en) * 1977-05-05 1988-06-08 Rolls Royce Nozzle guide vane structure for a gas turbine engine
US4194869A (en) * 1978-06-29 1980-03-25 United Technologies Corporation Stator vane cluster
US4248569A (en) * 1978-11-13 1981-02-03 General Motors Corporation Stator mounting
US4767267A (en) * 1986-12-03 1988-08-30 General Electric Company Seal assembly
US4721434A (en) * 1986-12-03 1988-01-26 United Technologies Corporation Damping means for a stator
SE459683B (en) * 1987-11-19 1989-07-24 Abb Stal Ab GAS TURBIN WITH LINKING INSTALLATION OF A SEALING RING IN A LED ROVER WIRE
US5149250A (en) * 1991-02-28 1992-09-22 General Electric Company Gas turbine vane assembly seal and support system
CA2070511C (en) * 1991-07-22 2001-08-21 Steven Milo Toborg Turbine nozzle support
US5249921A (en) * 1991-12-23 1993-10-05 General Electric Company Compressor outlet guide vane support
US5271714A (en) * 1992-07-09 1993-12-21 General Electric Company Turbine nozzle support arrangement
US6179560B1 (en) * 1998-12-16 2001-01-30 United Technologies Corporation Turbomachinery module with improved maintainability
US6234750B1 (en) * 1999-03-12 2001-05-22 General Electric Company Interlocked compressor stator
ITMI991206A1 (en) * 1999-05-31 2000-12-01 Nuovo Pignone Spa SUPPORT AND BLOCKING DEVICE FOR NOZZLES OF A HIGH PRESSURE STAGE IN GAS TURBINES
US6290459B1 (en) * 1999-11-01 2001-09-18 General Electric Company Stationary flowpath components for gas turbine engines
US6425738B1 (en) * 2000-05-11 2002-07-30 General Electric Company Accordion nozzle
US7000406B2 (en) * 2003-12-03 2006-02-21 Pratt & Whitney Canada Corp. Gas turbine combustor sliding joint
US7229245B2 (en) * 2004-07-14 2007-06-12 Power Systems Mfg., Llc Vane platform rail configuration for reduced airfoil stress
US20060088409A1 (en) * 2004-10-21 2006-04-27 General Electric Company Grouped reaction nozzle tip shrouds with integrated seals
US20060245923A1 (en) * 2005-04-27 2006-11-02 General Electric Company Arcuate nozzle segment and related method of manufacture
US20070071605A1 (en) * 2005-09-23 2007-03-29 General Electric Company Integrated nozzle and bucket wheels for reaction steam turbine stationary components and related method
US7836702B2 (en) * 2006-09-15 2010-11-23 Pratt & Whitney Canada Corp. Gas turbine combustor exit duct and HP vane interface
US20090053045A1 (en) * 2007-08-22 2009-02-26 General Electric Company Turbine Shroud for Gas Turbine Assemblies and Processes for Forming the Shroud
US8226360B2 (en) * 2008-10-31 2012-07-24 General Electric Company Crenelated turbine nozzle
EP2211023A1 (en) * 2009-01-21 2010-07-28 Siemens Aktiengesellschaft Guide vane system for a turbomachine with segmented guide vane carrier
DE102009037620A1 (en) * 2009-08-14 2011-02-17 Mtu Aero Engines Gmbh flow machine
US9650903B2 (en) * 2009-08-28 2017-05-16 United Technologies Corporation Combustor turbine interface for a gas turbine engine
CN101858229A (en) * 2010-04-29 2010-10-13 中国燃气涡轮研究院 Engine hot-centering and force-bearing type guider
US9835171B2 (en) * 2010-08-20 2017-12-05 Siemens Energy, Inc. Vane carrier assembly
FR2984428B1 (en) * 2011-12-19 2018-12-07 Safran Aircraft Engines COMPRESSOR RECTIFIER FOR TURBOMACHINE.
EP2952688A1 (en) * 2014-06-02 2015-12-09 Siemens Aktiengesellschaft Method for assembling a stator stage of a gas turbine engine
CN107208491B (en) * 2014-11-03 2019-08-06 诺沃皮尼奥内股份有限公司 The section of the component of grade for turbine and corresponding manufacturing method
DE102017105760A1 (en) * 2017-03-17 2018-09-20 Man Diesel & Turbo Se Gas turbine, vane ring of a gas turbine and method of making the same
US20190078469A1 (en) * 2017-09-11 2019-03-14 United Technologies Corporation Fan exit stator assembly retention system
US10815832B2 (en) * 2018-06-19 2020-10-27 Raytheon Technologies Corporation Load transfer in turbine exhaust case
US11073033B2 (en) * 2018-10-18 2021-07-27 Honeywell International Inc. Stator attachment system for gas turbine engine
EP3805525A1 (en) 2019-10-09 2021-04-14 Rolls-Royce plc Turbine vane assembly incorporating ceramic matric composite materials
US11092022B2 (en) * 2019-11-04 2021-08-17 Raytheon Technologies Corporation Vane with chevron face
US11591921B1 (en) 2021-11-05 2023-02-28 Rolls-Royce Plc Ceramic matrix composite vane assembly
US11732596B2 (en) 2021-12-22 2023-08-22 Rolls-Royce Plc Ceramic matrix composite turbine vane assembly having minimalistic support spars

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2675672A (en) * 1954-04-20 Schsrner
US2510606A (en) * 1943-05-22 1950-06-06 Lockheed Aircraft Corp Turbine construction
FR961133A (en) * 1947-02-17 1950-05-05
FR965713A (en) * 1947-05-07 1950-09-20
US2942844A (en) * 1952-12-22 1960-06-28 Gen Motors Corp Turbine nozzle
US2945671A (en) * 1955-02-10 1960-07-19 Rolls Royce Bladed rotor constructions for fluid machines
DE1017420B (en) * 1955-02-28 1957-10-10 Canadian Patents Dev Gas turbine engine with a multi-stage turbine
US2799473A (en) * 1955-04-27 1957-07-16 Gen Electric Gas turbine nozzle ring
FR1326037A (en) * 1962-06-07 1963-05-03 Napier Aero Engines Ltd Turbine
US3142475A (en) * 1962-12-28 1964-07-28 Gen Electric Stator assembly

Also Published As

Publication number Publication date
GB1129410A (en) 1968-10-02
DE1476795B2 (en) 1971-01-21
US3302926A (en) 1967-02-07
DE1476795A1 (en) 1969-12-04

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